US1590778A - Gyroscopic stabilizer for ships - Google Patents
Gyroscopic stabilizer for ships Download PDFInfo
- Publication number
- US1590778A US1590778A US413414A US41341420A US1590778A US 1590778 A US1590778 A US 1590778A US 413414 A US413414 A US 413414A US 41341420 A US41341420 A US 41341420A US 1590778 A US1590778 A US 1590778A
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- Prior art keywords
- rotor
- liquid
- casing
- bearing
- pressure
- Prior art date
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- Expired - Lifetime
Links
- 239000003381 stabilizer Substances 0.000 title description 5
- 239000007788 liquid Substances 0.000 description 32
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 16
- 230000000284 resting effect Effects 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 210000004907 gland Anatomy 0.000 description 2
- IATOMHNNMDOQEO-UHFFFAOYSA-N 2-(diethylamino)ethyl 2-phenylpentanoate;hydrochloride Chemical compound Cl.CCN(CC)CCOC(=O)C(CCC)C1=CC=CC=C1 IATOMHNNMDOQEO-UHFFFAOYSA-N 0.000 description 1
- 101100096502 Danio rerio spring gene Proteins 0.000 description 1
- 101100001674 Emericella variicolor andI gene Proteins 0.000 description 1
- 241001125879 Gobio Species 0.000 description 1
- 101150080778 INPP5D gene Proteins 0.000 description 1
- 241000117250 Jassa Species 0.000 description 1
- 101100096504 Mus musculus Spring1 gene Proteins 0.000 description 1
- 101001044101 Rattus norvegicus Lipopolysaccharide-induced tumor necrosis factor-alpha factor homolog Proteins 0.000 description 1
- 101100426090 Rattus norvegicus Trim9 gene Proteins 0.000 description 1
- 241000287181 Sturnus vulgaris Species 0.000 description 1
- 101100096505 Xenopus laevis spring1 gene Proteins 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000008400 supply water Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B39/00—Equipment to decrease pitch, roll, or like unwanted vessel movements; Apparatus for indicating vessel attitude
- B63B39/04—Equipment to decrease pitch, roll, or like unwanted vessel movements; Apparatus for indicating vessel attitude to decrease vessel movements by using gyroscopes directly
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S277/00—Seal for a joint or juncture
- Y10S277/926—Seal including fluid pressure equalizing or balancing feature
Definitions
- narran stares ALEXANDER E. SCI-HEIN, OF BROOKLYN's ⁇ N lilV' YORK, ASSIGNOR T0 THE SPERRY GYROSCOPE COMPANY, OF BROOKLYN, NEW YORK, A CORPORATION NEW YORK.
- This invention relates to gyroscopic stabilizers for ships and more particularly to evacuated casings and to bearings for theV rotor.
- gyroscopic stabilizers In gyroscopic stabilizers the usual practice is to encase the rotor and its driving motor in a casing within which a vacuum is created to eliminate air friction upon the rotor. motor and the rotor bearings are also contained within the vacuum. This causes difculty in cooling the motor and bearings and in lubricating the bearings.
- One of the objects of this invention is to devise a method and means whereby the rotor may be enclosed in an evacuated casing without so enclosing the motor and bearings.
- the invention further relates to an improved means and mechanism for maintaining a seal between a rotating element and its journal frame, so that a diiference in atmospheric conditions may be maintained around the rotor, such as reduced pressure or an atmosphere of light gas or the like.
- Fig. 1 is a sectional side elevation of a gyroscopic rotor and casing showing the application of my invention.
- Fig. 2 is an enlarged detail of the water gland or sealing device.
- Fig. 3 is a sectional detail of the lower portion of the casing andrrotor supporting bearings.
- 1 represents the gyroscopic rotor and 2 the casing therefor having the usual gudgeons 2 adapted to support the gyroscope for oscillation about an aXis at an angle to the spinning axis of the rotor.
- the rotor is .shown mounted within said casing lon upper and lower radial bearings 3, 4 and thrust bearing 5.
- the latter bearing may be of the oil tilm type whichy is capable of sustaining extremely high pressures. This type of bearing, however, oifers considerable resistance to starting, owing to the fact that when at rest the oil isv pressed out from between the bearing surfaces, and
- the bearing 5 may be of the usual oil film bearing construction comprising an upper shoe or plate 8 secured at 9 to the lower end of the rotor shaft 10 and resting uponthe' bearing surfaces 11 of self adjusting blocks 12 which are pivotally mounted on a supporting member 13 which has a knife edge bearing (not shown) on .a plate 14 in turn having a knife edge bearing (not shown) at right angles to the aforementioned knife edge bearing, on the end member 15 forming an integral part of the casing 2.
- this bearing do not form any part of this invention further details thereof will not be necessary.
- extension shaft 16 Secured to plate 8 coaxial with shaft 10 is in extension shaft 16 which projects downwardly through central openings 17 in inembers 13 .and 14 and is provided at its lower end with a plate 18 against which the upper race 19 of ball bearing 7 is adapted to rest.
- the lower race 2O of this bearing is carried by a member 21,the lower portion 22 of which forms a piston fitting into a cylinder 23 integral with and having its lower end closed by the end wall 24 of a cap 25 secured at 26 to member 15 and consequently to the casing 2.
- Piston rings or packing 27 may be provided on piston 22.
- An oil pump 28 is shown .attached to cap and communicating through channels 29, 30 with the inside of cylinder 23. Said pump may receive oil from a reservoir 31 through channel 32.
- a pipe 33 provided4 with a valve 34 may run from the inside of cylinder 23 to the reservoir 31.
- the outside of cylinder 2,3 may be provided with screw threads 35 engaged by an internally threaded collar 36; said collar in turn being provided with gear teeth 37 meshing with a pinion 38 fixed on a shaft 39 reaching through and bearing in the end of cap 25.
- a lever 40 is fixed on said shaft and may be actumovement of member 21.
- lever 40 engages stop 4l it will serve to indicate that the rotor is resting on the oil lm be'aringand free from the ball bearing.
- Collar 36 ist-o support member 21 in the raised position to prevent lowering ⁇ of the rotor in the event of leakage of oil from cylinder 23.
- the casing 2 is show-n ⁇ as having inner walls 44, 45 reaching' inwardly close to 'the sides of the rotor 1 toward the shaft 10 thereof. Said walls are each provided with a vertical anda horizontal groove or channel 46, 47 (see also Fig'. 2) encircling shaft 1() and slightly displaced therefrom. Fixed on Vthe shaft is a'circumferential member 48 reachinginto channel 47 at 50 and having downward projections 49 reaching ⁇ into channel 4f. At Va suitable vpoint without the casinfr may be Apositioned a water or other fluid supply ⁇ p ar tment Y valve with channel 46 while asimilar conduit 62 may connect chamber '63 of the Valve with channel 47.
- the control valve 52 is provided with a stem 64 carrying'a valve head 65 adapted to close the passage 66 between chambers 58 and 61; a piston valve 67 closing communication between .pipe 56 and the interior of the-valve, and a piston head 68 held in the positionshown against stop 69 by a springf'() pressing againstv said cyiinder and the end 71 of the valve casing.
- ⁇ .Jassa 'e7 2 is shown sermittino water from A ftcr chamber 6l to flow into chamber 7 3.
- Vthe rotcrhas been started andhas'attained a predetermined speed lrnob 74 of valve V2 may be pressed in to close the openingv()l and uncover the opening 59.
- Pump 57 being afdapted'to supply water at a predetermined kpressure will cause the water to rise through conduit 60 and flow into channel 46.
- the vacuum in chamber 77 may be broken before the speed of the rotor becomes too low, so that the Water in the channels will run bac-k into tank 5l.
- a rotatable element a casing enclosing said element, a circumferential grooved member on said casing, a circumferential member on said element reaching intoV said grooved member, means for supplying liquid to said grooved niember in starting, means responsive to the centrifugal pressure of liquid in said grooved member for rendering said liquid supply means ineifective, and additionalmeans for supplying liquid to said grooved member during normal operation adapted to become operative when said first supply means becomes ineffective.
- a rotatable element a casing therefor, said casing being provided with a channel, a projection on said element movable in said channel, means for supplying liquid underpressure to said channel, additional means connecting said .channel with a liquid source, means controlled by the volume of liquid in said channel for closing said rst named means and opening said second named means.
- a casing normally operating at less than atmospheric pressure, an opening into said casing, a rotatable element reaching through said opening, means for sealing said opening including a grooved portion associated With said casing surrounding said element, a circumferential projection on said element reaching into said grooved portion, means for supplying liquid under pressure to said portion, means for shutting off said liquid supply in response to the pressure of the liquid in the groove and for connecting the groove to a liquid source under less head than the static head on the liquid in said grooved portion.
- a liquid seal for the casings of rotors operating under less than atmospheric pressure comprising a member rotatable With the rotor, a stationary grooved member on said casing and receiving said rotatable member, and a liquid supply tank at less head than said members for normally supplying said members with liquid.
- an element rotatable on a normally vertical axis, a casing enclosing said element and provided with a circumferential groove adapted to contain liquid to the second annular channel in said casing of less radius than said groove and under the same, a circumferential projection on said element reaching into said groove for imp'elling ⁇ liquid in the groove, said projection being provided with a flaring and slanting portion to cause the liquid to be forced with greater pressure against the Walls of said groove, and blades on said projection extending into said channel for increasing the rate of rotation of the liquid.
- a rotatable element an evacuated casing therefor, a liquid seal between said casing and said element, means for supplying liquid to said seal, means controlled by the centrifugal pressure of the liquid in said seal for shutting olf said supply means and additional means for supplying liquid to said seal adapted to become than the liquid in said seal, and means for operative when said iirsa';k supply meansV beshutting off said pressure supply in response 10 comes ineffective. to the centrifugal pressurelof the liquid in 8.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Dental Tools And Instruments Or Auxiliary Dental Instruments (AREA)
Description
June 29 192e. l Y 1,590,778
A155. scHElN v GYROSCOPIC sTABILzR -Fon sHIPs v Filed sept. 28. 1920' 2 snets-sn'eet 1 MyW June 29 1926. 1,590,778
A. E. SCHEIN GYROSCOPIC STABILIZER FOR SHIPS Filed sept. 2s. 1920- 2' sheets-sheet s? "my `itatented June 29, 1926.
narran stares ALEXANDER E. SCI-HEIN, OF BROOKLYN's `N lilV' YORK, ASSIGNOR T0 THE SPERRY GYROSCOPE COMPANY, OF BROOKLYN, NEW YORK, A CORPORATION NEW YORK.
GYROSCOIIC STABILIZER FOR SHIPS.
Application led September 28, 1920. Serial No. 413,414.
This invention relates to gyroscopic stabilizers for ships and more particularly to evacuated casings and to bearings for theV rotor.
In gyroscopic stabilizers the usual practice is to encase the rotor and its driving motor in a casing within which a vacuum is created to eliminate air friction upon the rotor. motor and the rotor bearings are also contained within the vacuum. This causes difculty in cooling the motor and bearings and in lubricating the bearings.
One of the objects of this invention is to devise a method and means whereby the rotor may be enclosed in an evacuated casing without so enclosing the motor and bearings. v
The invention further relates to an improved means and mechanism for maintaining a seal between a rotating element and its journal frame, so that a diiference in atmospheric conditions may be maintained around the rotor, such as reduced pressure or an atmosphere of light gas or the like.
Referring to the drawings wherein I have shown what I now consider the preferred form of myinvention:
Fig. 1 is a sectional side elevation of a gyroscopic rotor and casing showing the application of my invention.
Fig. 2 is an enlarged detail of the water gland or sealing device.
Fig. 3 is a sectional detail of the lower portion of the casing andrrotor supporting bearings.
In the drawings, 1 represents the gyroscopic rotor and 2 the casing therefor having the usual gudgeons 2 adapted to support the gyroscope for oscillation about an aXis at an angle to the spinning axis of the rotor. The rotor is .shown mounted within said casing lon upper and lower radial bearings 3, 4 and thrust bearing 5. The latter bearing may be of the oil tilm type whichy is capable of sustaining extremely high pressures. This type of bearing, however, oifers considerable resistance to starting, owing to the fact that when at rest the oil isv pressed out from between the bearing surfaces, and
in fact the oil film between said surfaces,
is not established until a given speed of rotation is attained. In order then to facilitate the starting ofthe rotor so that it may readily be accomplished by the motor 6 pro- Under this system the driving vided to maintain the rotation of the rotor I have .provided a knon-friction .bearing 7 which may carry the entire weight of the rotor. during the starting period, the load being transf-erred to the heavier bearing after a predetermined speed has been attained.
The bearing 5 may be of the usual oil film bearing construction comprising an upper shoe or plate 8 secured at 9 to the lower end of the rotor shaft 10 and resting uponthe' bearing surfaces 11 of self adjusting blocks 12 which are pivotally mounted on a supporting member 13 which has a knife edge bearing (not shown) on .a plate 14 in turn having a knife edge bearing (not shown) at right angles to the aforementioned knife edge bearing, on the end member 15 forming an integral part of the casing 2. As the details of this bearing do not form any part of this invention further details thereof will not be necessary.
Secured to plate 8 coaxial with shaft 10 is in extension shaft 16 which projects downwardly through central openings 17 in inembers 13 .and 14 and is provided at its lower end with a plate 18 against which the upper race 19 of ball bearing 7 is adapted to rest. The lower race 2O of this bearing is carried by a member 21,the lower portion 22 of which forms a piston fitting into a cylinder 23 integral with and having its lower end closed by the end wall 24 of a cap 25 secured at 26 to member 15 and consequently to the casing 2. Piston rings or packing 27 may be provided on piston 22.
An oil pump 28 is shown .attached to cap and communicating through channels 29, 30 with the inside of cylinder 23. Said pump may receive oil from a reservoir 31 through channel 32. A pipe 33 provided4 with a valve 34 may run from the inside of cylinder 23 to the reservoir 31. The outside of cylinder 2,3 may be provided with screw threads 35 engaged by an internally threaded collar 36; said collar in turn being provided with gear teeth 37 meshing with a pinion 38 fixed on a shaft 39 reaching through and bearing in the end of cap 25. A lever 40 is fixed on said shaft and may be actumovement of member 21.
race `19 into erigagementy with plate 18. Continued actuation of said pump will raise the rotor 1 and dieengage the bearing surfaces of the oil lin bearing 5. lThe rot-'or will now be resting' wholly on the 'nonfriction ball bearing 7 ready for starting. l/Vhilepump 28 is being actuated lever 40 may be readily turned; since the weight is at that time removed from the threads, thereby causing collar 36 to follow-` the upward When lever 40 reaches stop 42 therotor'will have been raised to the proper position. Said lever will thus serve to indicate that the rotor is riding on the ball bearing' and entirely free from the friction bearing. Conversely, when lever 40 engages stop 4l it will serve to indicate that the rotor is resting on the oil lm be'aringand free from the ball bearing. Another important function of Collar 36 ist-o support member 21 in the raised position to prevent lowering `of the rotor in the event of leakage of oil from cylinder 23. Y
When the rotor has attained a speed sufficient to canse proper functioning cf bearing V5, the bearing 7 may be lowered to its inoperative position and the rotor will rest 'on bearing' 5.V To lower .the rotor a strolie of pump 28 may be necessary to ease collar 36 from the pressure of member 21. Lever 40 may then :be thrown around to stop 4l, rotating collar 86 on threads 85 'and lowering;` it toits inoperative position. Valve 34 may then Ybe turned to permit the oil in cylinder 23 to flow back into reservoir 3l. Obviously,` the passai'ge` through valve 34 maybe sulliciently small to canse a slow transfer of the `oil so that the raised ele ments will not be permitted todrop suddenly'tov their lower positions. The above Ydescribed specific form of thrust bea-ring is not claimed herein, however, but is reserved for copending application No. 43,462 for improvements 4in thrust bearings, filed duly 14,1925. i
The casing 2 is show-n` as having inner walls 44, 45 reaching' inwardly close to 'the sides of the rotor 1 toward the shaft 10 thereof. Said walls are each provided with a vertical anda horizontal groove or channel 46, 47 (see also Fig'. 2) encircling shaft 1() and slightly displaced therefrom. Fixed on Vthe shaft is a'circumferential member 48 reachinginto channel 47 at 50 and having downward projections 49 reaching` into channel 4f. At Va suitable vpoint without the casinfr may be Apositioned a water or other fluid supply` p ar tment Y valve with channel 46 while asimilar conduit 62 may connect chamber '63 of the Valve with channel 47. The control valve 52 is provided with a stem 64 carrying'a valve head 65 adapted to close the passage 66 between chambers 58 and 61; a piston valve 67 closing communication between .pipe 56 and the interior of the-valve, and a piston head 68 held in the positionshown against stop 69 by a springf'() pressing againstv said cyiinder and the end 71 of the valve casing. A
`.Jassa 'e7 2 is shown sermittino water from A ftcr chamber 6l to flow into chamber 7 3.
Vthe rotcrhas been started andhas'attained a predetermined speed lrnob 74 of valve V2 may be pressed in to close the openingv()l and uncover the opening 59. Pump 57 being afdapted'to supply water at a predetermined kpressure will cause the water to rise through conduit 60 and flow into channel 46. rl`he water inthe valve will pass through passage 72 into chamber 73 so that the pressure on the opposite ends of stopper will be e'qu-alized, while the pressure against valve head from within chamber 61 will br less than that against piston 68 from within chamber 73 by reason of the difference in area of these two elements, so/that the water pressure will serve to hold the valve ste-m 64 and integral parts in the inwardly pressed position even against the pressure of spr-ing 70, the strength of which is not sufficient Vto overcome the said difference in wat-er pressure. rllfhus when llrnob 74 has been pressed Y in and released the parts will remain-in this termined point represented yby dotted line 76, at which 'point the pressure vacting through conduit 62 and in chamber 63 of valve 52 due Ito the centrifugal force of the waterin channel 47 -1is designed to 'overcome the pressure on the rea-r side of Episton 68 andI force stem 64 back v to normal position, as shown, closing ,pipe 56 and openingpassage 66. In the meanwhile it will be seen that the water vin channels 46, l47 will have tightly sealed `the rotor within the linner compartment 77 of casing` 2 and preferably before valve 52 is restored to normal condition theiair should be withdrawn from com- 7 7 through tube 78 bylanv suitable apparatus so as to create a vacuum within said compartment.
'loo
After the vacuum'has'been established and in the manner set forth, communication between tank 51 and channel 4G Will have become established through pipe 54, chambers 53, 6l of the valve and conduit 60. The vacuum in the rotor chamber 'T7 will now tend to suck in the Water from the channels a6, il or in other Words, atmospheric pressure from Without Will tend to force the said Water into the vacuum chamber, While atmospheric pressure Will also tend to force Water from tank 5l into channel 46. vBotti of these tendencies Will be counteracted, however, by centrifugal force acting upon the Water in the channels.
Obviously the Water in the channels will in time decrease by evaporation or other causes so that the consequent decreased centrifugal force acting through conduit 60 will be overcome by the atmospheric pressure acting upon the Water 55, and Water will be forced from tank 51 into channel i6 until the balance is again established. Thus the sealing. Water gland in channels 4 6, l? will be automatically maintained.
`When it is desired to stop the rotor the vacuum in chamber 77 may be broken before the speed of the rotor becomes too low, so that the Water in the channels will run bac-k into tank 5l.
In accordance with the provisions of the patent statutes, I have herein described the principle of operation of my invention, together With the apparatus, Which I novv consider to represent the best embodiment thereof, but I desire to have it understood that the apparatus shown is only illustrative and that the invention can be carried out by other ine-ans.l Also, While it is designed to use the various features and elements in the combination and relations described, some of these may be altered and others omitted Without interfering with the more general results outlined, and the invention extends to such use.
Having described my invention, What I claim and desire to secure by Letters Patent is:
l. The combination with a rotatable element and a casing therefor, the operating pressure therein being normally less than atmospheric pressure, of a circumferentially grooved member on said casing, an annular projection carried by said element and entering said grooved member, and means for supplying liquid to said member at less than atmospheric pressure, the amount of liquid flowing into said member being governed by the balance between the negative pressure Within the casing and the pressure created by the centrifugal force of the rotating liquid.
2. In combination, a rotatable element, a casing enclosing said element, a circumferential grooved member on said casing, a circumferential member on said element reaching intoV said grooved member, means for supplying liquid to said grooved niember in starting, means responsive to the centrifugal pressure of liquid in said grooved member for rendering said liquid supply means ineifective, and additionalmeans for supplying liquid to said grooved member during normal operation adapted to become operative when said first supply means becomes ineffective. j
3. In combination, a rotatable element, a casing therefor, said casing being provided with a channel, a projection on said element movable in said channel, means for supplying liquid underpressure to said channel, additional means connecting said .channel with a liquid source, means controlled by the volume of liquid in said channel for closing said rst named means and opening said second named means.
4t. In combination, a casing normally operating at less than atmospheric pressure, an opening into said casing, a rotatable element reaching through said opening, means for sealing said opening including a grooved portion associated With said casing surrounding said element, a circumferential projection on said element reaching into said grooved portion, means for supplying liquid under pressure to said portion, means for shutting off said liquid supply in response to the pressure of the liquid in the groove and for connecting the groove to a liquid source under less head than the static head on the liquid in said grooved portion.
5. A liquid seal for the casings of rotors operating under less than atmospheric pressure comprising a member rotatable With the rotor, a stationary grooved member on said casing and receiving said rotatable member, and a liquid supply tank at less head than said members for normally supplying said members with liquid. A
6. In combination, an element rotatable on a normally vertical axis, a casing enclosing said element and provided with a circumferential groove adapted to contain liquid to the second annular channel in said casing of less radius than said groove and under the same, a circumferential projection on said element reaching into said groove for imp'elling` liquid in the groove, said projection being provided with a flaring and slanting portion to cause the liquid to be forced with greater pressure against the Walls of said groove, and blades on said projection extending into said channel for increasing the rate of rotation of the liquid.
7. In combination, a rotatable element, an evacuated casing therefor, a liquid seal between said casing and said element, means for supplying liquid to said seal, means controlled by the centrifugal pressure of the liquid in said seal for shutting olf said supply means and additional means for supplying liquid to said seal adapted to become than the liquid in said seal, and means for operative when said iirsa';k supply meansV beshutting off said pressure supply in response 10 comes ineffective. to the centrifugal pressurelof the liquid in 8. In combination, a rotatable element, an the seal and for connecting the seal to said evacuated easing therefor, a liquid seal besecond source of liquid. tween said easing and Said element, means In testimony whereof I have affixed my for supplying liquid to Said sea-l under pres-v signature. sure, e source of liquid under lese Statie head ALEXANDER E. SCHEIN.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US413414A US1590778A (en) | 1920-09-28 | 1920-09-28 | Gyroscopic stabilizer for ships |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US413414A US1590778A (en) | 1920-09-28 | 1920-09-28 | Gyroscopic stabilizer for ships |
Publications (1)
Publication Number | Publication Date |
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US1590778A true US1590778A (en) | 1926-06-29 |
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Family Applications (1)
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US413414A Expired - Lifetime US1590778A (en) | 1920-09-28 | 1920-09-28 | Gyroscopic stabilizer for ships |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2505391A (en) * | 1947-06-23 | 1950-04-25 | Jr Frank H Fletcher | Seal for centrifugal machines |
US2717182A (en) * | 1945-06-11 | 1955-09-06 | Daniel And Florence Guggenheim | Shaft-positioning mechanism for turbine-driven pumps |
US4447061A (en) * | 1982-06-04 | 1984-05-08 | Allied Corporation | Melt pump seal with vacuum housing |
EP1639314A1 (en) * | 2003-06-04 | 2006-03-29 | Gearloose Engineering, LLC | Gyroscopic roll stabilizer for boats |
WO2021174315A1 (en) * | 2020-03-06 | 2021-09-10 | Veem Ltd | Gyrostabiliser assembly |
US11428530B2 (en) * | 2018-05-24 | 2022-08-30 | Smartgyro S.R.L. | Gyroscope, support device, anti-roll stabilizer, vessel, use of a gyroscope, and method of servicing or maintaining a gyroscope |
US11801923B2 (en) | 2018-05-31 | 2023-10-31 | Wavetamer Llc | Gyroscopic boat roll stabilizer |
US11873064B2 (en) | 2020-03-02 | 2024-01-16 | Wavetamer Llc | Gyroscopic boat roll stabilizer with bearing cooling |
-
1920
- 1920-09-28 US US413414A patent/US1590778A/en not_active Expired - Lifetime
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2717182A (en) * | 1945-06-11 | 1955-09-06 | Daniel And Florence Guggenheim | Shaft-positioning mechanism for turbine-driven pumps |
US2505391A (en) * | 1947-06-23 | 1950-04-25 | Jr Frank H Fletcher | Seal for centrifugal machines |
US4447061A (en) * | 1982-06-04 | 1984-05-08 | Allied Corporation | Melt pump seal with vacuum housing |
EP1639314A1 (en) * | 2003-06-04 | 2006-03-29 | Gearloose Engineering, LLC | Gyroscopic roll stabilizer for boats |
EP1639314A4 (en) * | 2003-06-04 | 2010-03-31 | Seakeeper Inc | Gyroscopic roll stabilizer for boats |
US11428530B2 (en) * | 2018-05-24 | 2022-08-30 | Smartgyro S.R.L. | Gyroscope, support device, anti-roll stabilizer, vessel, use of a gyroscope, and method of servicing or maintaining a gyroscope |
US11698255B2 (en) | 2018-05-24 | 2023-07-11 | Smartgyro S.R.L. | Gyroscope, support device, anti-roll stabilizer, vessel, use of a gyroscope, and method of servicing or maintaining a gyroscope |
US11801923B2 (en) | 2018-05-31 | 2023-10-31 | Wavetamer Llc | Gyroscopic boat roll stabilizer |
US20240059381A1 (en) * | 2018-05-31 | 2024-02-22 | Wavetamer Llc | Gyroscopic Boat Roll Stabilizer |
US11873064B2 (en) | 2020-03-02 | 2024-01-16 | Wavetamer Llc | Gyroscopic boat roll stabilizer with bearing cooling |
WO2021174315A1 (en) * | 2020-03-06 | 2021-09-10 | Veem Ltd | Gyrostabiliser assembly |
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